Minh Chau Thi Pham
Examiner (ID: 10502, Phone: (571)272-1163 , Office: P/1776 )
Most Active Art Unit | 1776 |
Art Unit(s) | 1773, 1724, 3621, 1776, 1305, 1797 |
Total Applications | 2849 |
Issued Applications | 2227 |
Pending Applications | 153 |
Abandoned Applications | 469 |
Applications
Application number | Title of the application | Filing Date | Status |
---|---|---|---|
Array
(
[id] => 10806185
[patent_doc_number] => 20160152344
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-06-02
[patent_title] => 'FIRE EXTINCTION DESIGN FOR AN AUXILIARY POWER UNIT COMPARTMENT OF AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 14/951576
[patent_app_country] => US
[patent_app_date] => 2015-11-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2440
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14951576
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/951576 | Fire extinction design for an auxiliary power unit compartment of an aircraft | Nov 24, 2015 | Issued |
Array
(
[id] => 10806158
[patent_doc_number] => 20160152315
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-06-02
[patent_title] => 'AIRCRAFT FUSELAGE FRAME'
[patent_app_type] => utility
[patent_app_number] => 14/952376
[patent_app_country] => US
[patent_app_date] => 2015-11-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14952376
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/952376 | Aircraft fuselage frame | Nov 24, 2015 | Issued |
Array
(
[id] => 10798790
[patent_doc_number] => 20160144947
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-05-26
[patent_title] => 'HIGH-LIFT SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/948765
[patent_app_country] => US
[patent_app_date] => 2015-11-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 2037
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14948765
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/948765 | High-lift system | Nov 22, 2015 | Issued |
Array
(
[id] => 11648863
[patent_doc_number] => 20170144764
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-05-25
[patent_title] => 'INTEGRATED AIRCRAFT SEAT AND SIDEWALL'
[patent_app_type] => utility
[patent_app_number] => 14/949081
[patent_app_country] => US
[patent_app_date] => 2015-11-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 2000
[patent_no_of_claims] => 18
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/949081 | INTEGRATED AIRCRAFT SEAT AND SIDEWALL | Nov 22, 2015 | Abandoned |
Array
(
[id] => 11536645
[patent_doc_number] => 09611042
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2017-04-04
[patent_title] => 'System for securing an aircraft door'
[patent_app_type] => utility
[patent_app_number] => 14/945755
[patent_app_country] => US
[patent_app_date] => 2015-11-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 3202
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14945755
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/945755 | System for securing an aircraft door | Nov 18, 2015 | Issued |
Array
(
[id] => 12285385
[patent_doc_number] => 09932117
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2018-04-03
[patent_title] => 4-bar side canopy release
[patent_app_type] => utility
[patent_app_number] => 14/945799
[patent_app_country] => US
[patent_app_date] => 2015-11-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14945799
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/945799 | 4-bar side canopy release | Nov 18, 2015 | Issued |
Array
(
[id] => 13036859
[patent_doc_number] => 10040547
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2018-08-07
[patent_title] => Unmanned aerial vehicle
[patent_app_type] => utility
[patent_app_number] => 14/944418
[patent_app_country] => US
[patent_app_date] => 2015-11-18
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14944418
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/944418 | Unmanned aerial vehicle | Nov 17, 2015 | Issued |
Array
(
[id] => 10663253
[patent_doc_number] => 20160009397
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-01-14
[patent_title] => 'VEHICLE OCCUPANT SUPPORT'
[patent_app_type] => utility
[patent_app_number] => 14/852593
[patent_app_country] => US
[patent_app_date] => 2015-09-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 21
[patent_figures_cnt] => 21
[patent_no_of_words] => 12214
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 9
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14852593
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/852593 | Vehicle occupant support | Sep 12, 2015 | Issued |
Array
(
[id] => 16429151
[patent_doc_number] => 10829217
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-11-10
[patent_title] => Light-limiting header assembly for a transition area within an interior cabin of an aircraft
[patent_app_type] => utility
[patent_app_number] => 14/835850
[patent_app_country] => US
[patent_app_date] => 2015-08-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
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[patent_no_of_words] => 7715
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14835850
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/835850 | Light-limiting header assembly for a transition area within an interior cabin of an aircraft | Aug 25, 2015 | Issued |
Array
(
[id] => 10475783
[patent_doc_number] => 20150360799
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-17
[patent_title] => 'High-Speed Airplane Deicing Installation Systems and Methods'
[patent_app_type] => utility
[patent_app_number] => 14/833564
[patent_app_country] => US
[patent_app_date] => 2015-08-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 36
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14833564
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/833564 | High-speed airplane deicing installation systems and methods | Aug 23, 2015 | Issued |
Array
(
[id] => 10801075
[patent_doc_number] => 20160147232
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-05-26
[patent_title] => 'UNMANNED AERIAL VEHICLE DRAG AUGMENTATION BY REVERSE PROPELLER ROTATION'
[patent_app_type] => utility
[patent_app_number] => 14/810386
[patent_app_country] => US
[patent_app_date] => 2015-07-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14810386
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/810386 | Unmanned aerial vehicle drag augmentation by reverse propeller rotation | Jul 26, 2015 | Issued |
Array
(
[id] => 10677599
[patent_doc_number] => 20160023745
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-01-28
[patent_title] => 'SEALING ASSEMBLY ON THE EXTERIOR OF AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 14/806878
[patent_app_country] => US
[patent_app_date] => 2015-07-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 2784
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14806878
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/806878 | SEALING ASSEMBLY ON THE EXTERIOR OF AN AIRCRAFT | Jul 22, 2015 | Abandoned |
Array
(
[id] => 13064873
[patent_doc_number] => 10053209
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-08-21
[patent_title] => Aircraft winglet design having a compound curve profile
[patent_app_type] => utility
[patent_app_number] => 14/807579
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/807579 | Aircraft winglet design having a compound curve profile | Jul 22, 2015 | Issued |
Array
(
[id] => 11396705
[patent_doc_number] => 20170017241
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-01-19
[patent_title] => 'Pilot Assistance System'
[patent_app_type] => utility
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[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/800346 | Pilot assistance system | Jul 14, 2015 | Issued |
Array
(
[id] => 10614614
[patent_doc_number] => 09334044
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-05-10
[patent_title] => 'Method for generating hydraulic power in an aircraft, use of a hybrid power control unit and drive system'
[patent_app_type] => utility
[patent_app_number] => 14/797527
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/797527 | Method for generating hydraulic power in an aircraft, use of a hybrid power control unit and drive system | Jul 12, 2015 | Issued |
Array
(
[id] => 10677608
[patent_doc_number] => 20160023753
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-01-28
[patent_title] => 'VEHICLE WITH ASYMMETRIC NACELLE CONFIGURATION'
[patent_app_type] => utility
[patent_app_number] => 14/795505
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/795505 | Vehicle with asymmetric nacelle configuration | Jul 8, 2015 | Issued |
Array
(
[id] => 11382565
[patent_doc_number] => 20170008622
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-01-12
[patent_title] => 'AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 14/795406
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14795406
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/795406 | Aircraft | Jul 8, 2015 | Issued |
Array
(
[id] => 10657810
[patent_doc_number] => 20160003954
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-01-07
[patent_title] => 'AERIAL VEHICLE ACQUISITION OF SEISMIC DATA'
[patent_app_type] => utility
[patent_app_number] => 14/793520
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/793520 | AERIAL VEHICLE ACQUISITION OF SEISMIC DATA | Jul 6, 2015 | Abandoned |
Array
(
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[patent_country] => US
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[patent_issue_date] => 2016-03-10
[patent_title] => 'Unmanned Aircraft Systems Ground Support Platform'
[patent_app_type] => utility
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Array
(
[id] => 14730747
[patent_doc_number] => 10384760
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-08-20
[patent_title] => Self-adjusting door jamb for an aircraft door
[patent_app_type] => utility
[patent_app_number] => 14/792231
[patent_app_country] => US
[patent_app_date] => 2015-07-06
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/792231 | Self-adjusting door jamb for an aircraft door | Jul 5, 2015 | Issued |